View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58196U 26145.13105076 +.00000000 +00000-0 -56145-4 0 00009
2 58196 43.0032 71.8822 0001745 271.1636 88.9016 15.27586588 01
| Epoch (UTC): | 25 May 2026 03:08:42 |
| Eccentricity: | 0.0001745 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.8822° |
| argument of perigee: | 271.1636° |
| revolutions per day: | 15.27586588 |
| mean anomaly at epoch: | 88.9016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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